Hybrid coordinate formulation for flexible space vehicle attitude control system design


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    Title :

    Results of flexible spacecraft attitude control studies utilizing hybrid coordinates


    Contributors:

    Conference:

    AEROSPACE SCIENCES MEETING ; 1970 ; NEW YORK, NY


    Publication date :

    1971-03-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :